orbit operations checklist - nasafs iii orb ops/135/fin 1 orbit operations checklist sts-135 flight...

JSC-48036-135

Orbit Operations Checklist

STS-135 Flight Supplement

Mission Operations Directorate Operations Division

Final April 11, 2011

National Aeronautics and Space Administration

Lyndon B. Johnson Space Center Houston, Texas Verify this is the correct version for the pending operation (training, simulation or flight). Electronic copies of FDF books are available. URL: http://mod.jsc.nasa.gov/do3/FDF/index.html

FS ii ORB OPS/135/FIN

Incorporates the following: 482#: ORB OPS FS-00235 ORB OPS FS-00238 ORB OPS FS-00236 ORB OPS FS-00239 ORB OPS FS-00237A(S) S – Superseded

AREAS OF TECHNICAL RESPONSIBILITY

Publication Manager DO3/T. Zulauf 281-244-0922 Alternate Publication Manager

DO3/A. Blaylock 281-244-1184

COMM/INST DS2/H. Brewer 281-483-7208 PTG DO4/M. Mendoza 281-483-0787 DAP TABLES DS6/A. Prasse 281-483-3616 REBOOST/DAP DS6/A. Prasse 281-483-3616 OIU DS2/H. Brewer 281-483-7208 SDBI SK/S. Irwin 281-218-3071 WLES DO5/R. Besser 281-244-5627 P/L OF OPP DS6/A. Prasse 281-483-3616 CWC OPS DX4/O. Abotteen 281-483-2703 PGSC FS DO4/T. Melroy 281-244-1132 CUE CARDS: LIOH CHANGEOUT DS4/K. Wollard 281-483-3815 ORBIT BURN MONITOR DS6/L. Schmitt 281-483-0694 DAP TABLES DS6/A. Prasse 281-483-3616 MAUI FIRING SEQUENCES

DS6/A. Prasse 281-483-3616

WLES CONFIG AFTER PGSC REBOOT

DO5/R. Besser 281-244-5627

FS iii ORB OPS/135/FIN 1

ORBIT OPERATIONS CHECKLIST STS-135 FLIGHT SUPPLEMENT LIST OF EFFECTIVE PAGES

FINAL 04/11/11 PCN-1 06/16/11

Sign Off ........... * 135/FIN FS ii ................. * 135/FIN FS iii ................ * 135/FIN 1 FS iv ................ * 135/FIN 1 FS v ................. * 135/FIN 1 FS vi ................ * 135/FIN FS vii ............... 135/FIN 1 FS viii .............. 135/FIN FS 1-1 ............. 135/FIN FS 1-2 ............. 135/FIN FS 1-3 ............. 135/FIN FS 1-4 ............. 135/FIN FS 1-5 ............. 135/FIN FS 1-6 ............. 135/FIN FS 1-7 ............. 135/FIN FS 1-8 ............. 135/FIN FS 1-9 ............. 135/FIN FS 1-10 ........... 135/FIN FS 1-11 ........... 135/FIN FS 1-12 ........... 135/FIN FS 2-1 ............. 135/FIN 1 FS 2-2 ............. 135/FIN 1 FS 2-3 ............. 135/FIN 1 FS 2-4 ............. 135/FIN 1 FS 2-5 ............. 135/FIN 1 FS 2-6 ............. 135/FIN 1 FS 3-1 ............. 135/FIN FS 3-2 ............. 135/FIN FS 3-3 ............. 135/FIN FS 3-4 ............. 135/FIN

FS 3-5 .............. 135/FIN FS 3-6 .............. 135/FIN FS 3-7 .............. 135/FIN FS 3-8 .............. 135/FIN FS 4-1 .............. 135/FIN FS 4-2 .............. 135/FIN FS 4-3 .............. 135/FIN FS 4-4 .............. 135/FIN FS 4-5 .............. 135/FIN 1 FS 4-6 .............. 135/FIN FS 5-1 .............. 135/FIN FS 5-2 .............. 135/FIN FS 6-1 .............. 135/FIN FS 6-2 .............. 135/FIN 1 FS 7-1 .............. 135/FIN FS 7-2 .............. 135/FIN 1 FS 7-3 .............. 135/FIN FS 7-4 .............. 135/FIN FS 7-5 .............. 135/FIN FS 7-6 .............. 135/FIN FS 7-7 .............. 135/FIN FS 7-8 .............. 135/FIN FS 7-9 .............. 135/FIN FS 7-10 ............ 135/FIN FS 7-11 ............ 135/FIN 1 FS 7-12 ............ 135/FIN FS 7-13 ............ 135/FIN 1 FS 7-14 ............ 135/FIN 1 FS 7-15 ............ 135/FIN FS 7-16 ............ 135/FIN

* – Omit from flight book

FS iv ORB OPS/135/FIN 1

FS 7-17 ........... 135/FIN FS 7-18 ........... 135/FIN FS 7-19 ........... 135/FIN FS 7-20 ........... 135/FIN FS 7-21 ........... 135/FIN FS 7-22 ........... 135/FIN FS 7-23 ........... 135/FIN FS 7-24 ........... 135/FIN 1 FS 8-1 ............. 135/FIN FS 8-2 ............. 135/FIN FS 8-3 ............. 135/FIN FS 8-4 ............. 135/FIN FS 8-5 ............. 135/FIN FS 8-6 ............. 135/FIN FS 8-7 ............. 135/FIN FS 8-8 ............. 135/FIN FS 8-9 ............. 135/FIN FS 8-10 ........... 135/FIN FS 8-11 ........... 135/FIN FS 8-12 ........... 135/FIN FS 8-13 ........... 135/FIN FS 8-14 ........... 135/FIN 1 FS 8-15 ........... 135/FIN 1 FS 8-16 ........... 135/FIN 1 FS 8-17 ........... 135/FIN 1 FS 8-18 ........... 135/FIN FS 9-1 ............. 135/FIN FS 9-2 ............. 135/FIN FS 9-3 ............. 135/FIN FS 9-4 ............. 135/FIN FS 10-1 ........... 135/FIN FS 10-2 ........... 135/FIN FS 10-3 ........... 135/FIN FS 10-4 ........... 135/FIN FS 11-1 ........... * 135/FIN FS 11-2 ........... * 135/FIN FS CC 11-3 ..... * 135/FIN 1 FS CC 11-4 ..... * 135/FIN 1

FS CC 11-5 ...... * 135/FIN FS CC 11-6 ...... * 135/FIN FS CC 11-7 ...... * 135/FIN FS CC 11-8 ...... * 135/FIN FS CC 11-9 ...... * 135/FIN FS CC 11-10 .... * 135/FIN FS CC 11-11 .... * 135/FIN FS CC 11-12 .... * 135/FIN FS CC 11-13 .... * 135/FIN FS CC 11-14 .... * 135/FIN FS CC 11-15 .... * 135/FIN FS 11-16 .......... * 135/FIN

* – Omit from flight book

FS v ORB OPS/135/FIN 1

ORBIT OPS CUE CARDS

Title Ref. Page Card No.

LIOH CHANGEOUT (Front) .. FS CC 11-3 ORB OPS-29a/ nonRCRS/135/O/B LIOH CANISTER STOWAGE

LOCATIONS (Back) ............ FS CC 11-4 ORB OPS-29b/ nonRCRS/135/O/B ORBIT BURN MONITOR

(Front) .................................... FS CC 11-5 ORB OPS-31a/135/O/B OMS FAILURES

(Back) .................................... FS CC 11-6 ORB OPS-31b/135/O/A STS-135 DAP CONFIGURATIONS (Front/Top) ............................ FS CC 11-7 ORB OPS-41a/135/O/A (Front/Bottom) ...................... FS CC 11-8 ORB OPS-41aa/135/O/A (Back/Top) ............................ FS CC 11-9 ORB OPS-41b/135/O/B (Back/Bottom) ....................... FS CC 11-10 ORB OPS-41bb/135/O/B MAUI PRCS AND VRCS –

RCS FIRING SEQUENCE (Front) .................................... FS CC 11-11 ORB OPS-42a/135/O/A

MAUI PRCS ONLY FIRING SEQUENCE (Back of MAUI PRCS AND VRCS – RCS FIRING SEQUENCE).......... FS CC 11-12 ORB OPS-42aa/135/O/A

MAUI VRCS ONLY FIRING SEQUENCE

(Front) .................................... FS CC 11-13 ORB OPS-42b/135/O/A (Back) .................................... FS CC 11-14 ORB OPS-42bb/135/O/A WLES CONFIG AFTER PGSC REBOOT

(Front) .................................... FS CC 11-15 ORB OPS-47a/135/O/A

FS vi ORB OPS/135/FIN

This Page Intentionally Blank

FS vii ORB OPS/135/FIN

CONTENTS PAGE

COMM/INST ................................................................... FS 1-1 LOAD PCMMU FORMAT .......................................... FS 1-2 LOAD PDI DECOM FORMAT ................................... FS 1-4 LOAD OIU FORMAT/CONFIG .................................. FS 1-7 DOWNLINK OCA DATA VIA WIDE BAND ANALOG FM ........................................................... FS 1-9

PTG ................................................................................ FS 2-1

STAR PAIRS PAD (MET APPLICALBE: POST OMS2 – 006/00:00:00) .... FS 2-2

STAR PAIRS (MET APPLICALBE: POST OMS2 – 006/00:00:00) .... FS 2-3

STAR PAIRS PAD (MET APPLICABLE: 006/00:00:00 – NOMINAL EOM) . FS 2-4

STAR PAIRS (MET APPLICABLE: 006/00:00:00 – NOMINAL EOM) . FS 2-5

DAP TABLES ................................................................. FS 3-1

DAP OVERVIEW ....................................................... FS 3-2 UNIV PTG ................................................................. FS 3-3 STS-135 DAP A CONFIGURATIONS ....................... FS 3-4 STS-135 DAP B CONFIGURATIONS ....................... FS 3-6

REBOOST/DAP ............................................................. FS 4-1

AUTO REBOOST ...................................................... FS 4-2 AUTO REBOOST ATTITUDE REFERENCE ............ FS 4-4 DOCKED DAP REFERENCE ................................... FS 4-5 RATE DAMPING ....................................................... FS 4-5 ROBOTICS ATTITUDE MAINTENANCE .................. FS 4-6

OIU PROCEDURES ...................................................... FS 5-1

OIU ACTIVATION ..................................................... FS 5-2 OIU DEACTIVATION ................................................ FS 5-2

SHORT DURATION BIOASTRONAUTICS INVESTIGATION (SDBI) ............................................... FS 6-1

SDBI 1634, SLEEP-WAKE ACTIGRAPHY ............... FS 6-2

Cont next page ORB OPS/135/FIN 1

FS viii ORB OPS/135/FIN

WING LEADING EDGE SENSORS (WLES) PROCEDURES ............................................................ FS 7-1

WLES ACTIVATION AND CHECKOUT .................... FS 7-2 WLES DEACTIVATION AND TEARDOWN .............. FS 7-10 WLES LAPTOP RECEIVER UNIT (LRU) R&R ......... FS 7-12 WLES CABIN RELAY UNIT R&R ............................. FS 7-14 CONFIGURE WLES DATA FILE BACKUP PATH .... FS 7-16 PREP WLES LAPTOPS FOR TRANSFER ............... FS 7-17 WLES RNDZ TOOLS CHECKOUT PREP ................ FS 7-18 WLES DOCK/UNDOCK RECOVERY ....................... FS 7-18 DISABLE WLES FILE BACKUP ................................ FS 7-19 ENABLE WLES FILE BACKUP ................................. FS 7-19 LRU TROUBLESHOOTING ...................................... FS 7-20

PAYLOADS OF OPPORTUNITY ................................... FS 8-1

MAUI PRCS AND VRCS PROCEDURE ................... FS 8-2 MAUI VRCS ONLY PROCEDURE ............................ FS 8-6 MAUI PRCS ONLY PROCEDURE ............................ FS 8-10 RAMBO-2 PROCEDURE .......................................... FS 8-14

CWC OPS ...................................................................... FS 9-1

WASTE TANK OFFLOAD TO CWC ......................... FS 9-2 PGSC FS ....................................................................... FS 10-1

KFX DOWNLINK IN THE BLIND ............................... FS 10-2 CUE CARD CONFIGURATION ..................................... FS 11-1

FS 1-1 ORB OPS/135/FIN

COMM/INST

LOAD PCMMU FORMAT ............................................... FS 1-2 LOAD PDI DECOM FORMAT ........................................ FS 1-4 LOAD OIU FORMAT/CONFIG ....................................... FS 1-7 DOWNLINK OCA DATA VIA WIDE BAND ANALOG FM .. FS 1-9

CO

MM

/ IN

ST


LOAD PCMMU FORMAT

C3 1. √OI PCMMU FORMAT – GPC SM 62 PCMMU/PL COMM

2. FORMAT: CRT SEL FXD – ITEM 1 EXEC (*)

SEL ID – ITEM 3 +X X X EXEC 3. √SM COMM BUF – RDY

LOAD – ITEM 4 EXEC √LOAD, ITEM 4 – RUN,CPLT

If LOAD – CPLT:

Repeat steps 2 and 3 for second ID C3 CRT

* * * * * * * * * * * * * * *

If LOAD – FAIL and ERR MSG – ‘I/O ERR MMU 1(2)’:

Go to 5.2a, ‘I/O ERR MMU 1(2)’ (MAL, DPS) >>

If LOAD – FAIL and a first load attempt:

Repeat steps 2 and 3 for failed ID If LOAD – FAIL and a subsequent load attempt: √MCC

OI PCMMU PWR – 2(1) √ERR MSG – ‘I/O ERR PCM’

I/O RESET PCM – ITEM 5 EXEC (*) Repeat steps 2 and 3

* * * * * * * * * * * * * * *

4. When final LOAD – CPLT:

SEL PGM – ITEM 2 EXEC (*)

CO

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/ IN

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DNLIST COMPATIBILITY PHASE

FORMAT ID

64/128CONFIG

NO.

G1,G3,BFS (ASCENT) 102/FXD – G3,BFS (ENTRY) 102/164 – G2,G8,S2 ORBIT/ FCS C/O 103/161 – G2,S2,OPS 0 OPS 0 – /163 – G2,S2,P9 MMU C/O – /163 – G2,G8,S2 RNDZ w/UHF FMT CCSU

(SSOR/SSV/TCS) (PRIME) 103/192 763 G2,G8,S2 RNDZ w/UHF FMT CCSU

(SSOR/SSV/TCS) (B/U) 103/211 770 G2,G8,S2 DOCKED ISS FMT CCSH

(OIU/SSV) (PRIME) 103/184 760 G2,G8,S2 DOCKED ISS FMT CCSH

(OIU/SSV) (B/U) 103/205 767 G2,G8,S2 OIU C/O AND SSV RATE 4

(PRIME) 103/188 762 G2,G8,S2 OIU C/O AND SSV RATE 5

(B/U) 103/203 765 G2,G8,S2 MPLM FMT (OIU/SSV) (PRIME) 103/199 780 G2,G8,S2 MPLM FMT (OIU/SSV) (B/U) 103/212 781

NOTE LDR TFL may affect PCMMU BITE. If PCMMU or SM 2 GPC switched since last TFL, ID 64 and 128 will not reflect current state


LOAD PDI DECOM FORMAT

SM 62 PCMMU/PL COMM 1. PDI: CRT √I/O RESET – ITEM 8 (*)

SEL DECOM – ITEM 9 +X EXEC SEL FMT – ITEM 10 +X X X EXEC LOAD – ITEM 11 EXEC

If LOAD – CPLT:

SEL INPUT – ITEM 12 +X EXEC LOAD – ITEM 13 EXEC Repeat step 1 for additional DECOMs/FPM

A1L CRT

* * * * * * * * * * * * * * * * * * * * * * * * * * *

If LOAD – FAIL and ERR MSG – ‘I/O ERR MMU 1(2)’:

Go to 5.2a, ‘I/O ERR MMU 1(2)’ (MAL, DPS) >>

If LOAD – FAIL and a first load attempt:

Repeat step 1 If LOAD – FAIL and a subsequent load attempt:

NOTE

Power cycling PDI will cause PDI to lose DFLs previously loaded

√MCC

S-BD PL CNTL – PNL PL DATA INTLVR PWR – OFF,ON

√ERR MSG – ‘S62 BCE BYP PL’ √‘S62 BCE BYP PDI’ S-BD PL CNTL – CMD

PCM:

I/O RESET PCM – ITEM 5 EXEC (*) PDI:

I/O RESET – ITEM 8 EXEC (*) Repeat step 1 for all of config (XXX)

* * * * * * * * * * * * * * * * * * * * * * * * * * *


CONFIG DECOM FMT INPUT USE 763

RNDZ w/UHF FMT CCSU

(PRIME) TFL 192

12 3 4

5-FPM

30– 9 4

505

1,2– 5 4

OIU7 (CCSU) ** –

TCS SSV (3) ***

H-H-H *

770 RNDZ w/UHF FMT CCSU

(BACKUP) TFL 211

12 3 4

5-FPM

1431 – 19 503

41,2 – 5

SSV (3) *** OIU7 (CCSU) **

– TCS

H-H-H *

760 DOCKED FMT

CCSH

(PRIME) TFL 184

12 3 4

5-FPM

7– – 27 501

1,2– – 4

OIU9 (CCSH) ** – –

SSV (2) ***

H-H-H * 767

DOCKED FMT CCSH

(BACKUP) TFL 205

12 3 4

5-FPM

–17 29 –

508

–1,2 4 –

–OIU9 (CCSH) **

SSV (2) *** –

H-H-H * 762

SSV RATE 4

(PRIME) TFL 188

12 3 4

5-FPM

5– – 1

507

1,2– – 4

OIU255 ** – –

SSV (4) ***

H-H-H * 765

SSV RATE 5

(BACKUP) TFL 203

12 3 4

5-FPM

–15 11 –

509

–1,2 4 –

– OIU255 ** SSV (5) ***

–

L-H-H * * OI-GNC-SM, Orbiter Downlist Data Rates (High or Low) ** # in OIU# represents the OIU format; (XXX) represents data type *** # in SSV (#) represents the SSV Out Rate sw selection

Cont next page


780 MPLM FMT

(PRIME) TFL 199

12 3 4

5-FPM

2– – 4

504

1,2– – 4

OIU5 (1M) ** – –

SSV (3) ***

H-H-H * 781

MPLM FMT

(BACKUP) TFL 212

12 3 4

5-FPM

143 – –

502

41,2 – –

SSV (3) *** OIU5 (1M) **

– –

H-H-H * * OI-GNC-SM, Orbiter Downlist Data Rates (High or Low) ** # in OIU# represents the OIU format; (XXX) represents data type *** # in SSV (#) represents the SSV Out Rate sw selection


LOAD OIU FORMAT/CONFIG Determine which step is needed and complete all actions to obtain desired OIU configuration

NOTE

A corresponding TFL/DFL CONFIG is reqd for MCC to receive telemetry. Reference S62 PCMMU/PL COMM for the last loaded HDR TFL and perform LOAD PCMMU FORMAT/LOAD PDI DECOM FORMAT for the associated CONFIG

S212 OIU

1. GNC-1 PRIMARY ON LB-ORB N2-1 (OIU BUS 3)

LOAD FORMAT ITEM 1 +9 EXEC GNC TO GNC 1 ITEM 18 +1 4 EXEC GNC 1 TO BUS 3 ITEM 18 +1 6 EXEC BUS 4 BC ITEM 15 EXEC (*) BUS 3 RT ITEM 10 EXEC (*) LOAD FORMAT ITEM 1 +9 EXEC >>







Cont next page


5. MPLM LOAD FORMAT ITEM 1 +5 EXEC BUS 2 BC ITEM 7 EXEC (*) LOAD FORMAT ITEM 1 +5 EXEC >>

6. SSOR

LOAD FORMAT ITEM 1 +7 EXEC BUS 1 BC ITEM 3 EXEC (*) LOAD FORMAT ITEM 1 +7 EXEC >>


DOWNLINK OCA DATA VIA WIDE BAND ANALOG FM (35 min)

OBJECTIVE: Downlink OCA data via S-band system LOCATION: Payload Station on aft Flight Deck (L10:A1), PDIP1 (L12) TOOLS REQD: TOOL Gray Tape Kapton Tape Pin Kit (Test Jumper Leads) MISC Sharpie 1. Obtain two, 5-in 22-ga Pin/Socket Test Jumper

Leads from the Pin Kit L10:A1 2. Open locker door, locate “Bottom of Locker Cable”

(see diagram below) 3. Demate Dnlk Y Cable (SED39127625-301) from

Bottom of Locker Cable P2 (see diagram below)

Middeck 4. Power down the OCA Router L12 5. Locate OCA INTF Cable (SED16103948-301) plug

P2 mated to J4 on PDIP1 6. Demate OCA INTF Cable plug P2 from J4

Re-route OCA INTF Cable plug P2 near L10A1 to allow jumper installation in following steps (remove pre-route ties as necessary)

Cont next page


L10:A1 7. Obtain Test Jumper Leads, mark both ends of one Lead using Sharpie

8. Twist Test Jumper Leads together to form a twisted

pair (see diagram below) 9. Per the drawing below, install Test Jumper Lead

twisted pair between the Bottom of Locker Cable plug P2 and the OCA INTF Cable plug P2 (ensure Sharpie marked Test Jumper Lead is connected between socket 1 and pin 15)

10. Using Kapton Tape, secure Test Jumper Lead/plug

connections, cover unused pins/sockets on plugs 11. Ensure connector shells are in contact for chassis

ground 12. Using Gray Tape, secure cables, plugs, jumpers

Secure locker door as required (use caution not to pinch wiring)

Middeck 13. Power on the OCA Router 14. Stow tools

5-in, 22-ga Test Jumper Lead twisted pair

Sharpie marked Test Jumper Lead

Bottom of Locker Cable plug P2 OCA INTF Cable plug P2

Cont next page


When OCA downlink no longer required: Middeck 15. Power down the OCA Router L10:A1 16. Remove Gray Tape, Kapton Tape as required 17. Remove Test Jumper Leads from Bottom of

Locker Cable and OCA INTF Cable plugs 18. Mate Dnlk Y Cable (SED39127625-301) to

Bottom of Locker Cable plug P2 L12 19. Re-route OCA INTF Cable plug P2 to PDIP1 20. Mate OCA INTF Cable plug P2 to J4 on PDIP1 21. Stow tools

FS 2-1 ORB OPS/135/FIN 1

PTG

STAR PAIRS PAD (MET APPLICABLE: POST OMS2 – 006/00:00:00) .......... FS 2-2

STAR PAIRS (MET APPLICABLE: POST OMS2 – 006/00:00:00) .......... FS 2-3

STAR PAIRS PAD (MET APPLICABLE: 006/00:00:00 – NOMINAL EOM) ...... FS 2-4

STAR PAIRS (MET APPLICABLE: 006/00:00:00 – NOMINAL EOM) ...... FS 2-5

PTG

FS

2-2 O

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OP

S/135/FIN

1

STAR

PAIR

S PAD

PTG


STAR PAIRS

FS

2-4 O

RB

OP

S/135/FIN

1

STAR

PAIR

S PAD


STAR PAIRS


DAP TABLES

DAP OVERVIEW ........................................................... FS 3-2 UNIV PTG ...................................................................... FS 3-3 STS-135 DAP A CONFIGURATIONS ............................ FS 3-4 STS-135 DAP B CONFIGURATIONS ............................ FS 3-6

DA

P TA

BLE

S

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3-2 O

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S/135/FIN

DAP OVERVIEW DAP – Purpose DAP – Purpose

A1 – Nominal B1 – OMS & RCS Burns (ORB OPS) A2 – PTC B2 – Loss of VERN (Tail Only) A3 – GG B3 – Loss of VERN (All) A4 – B4 – A5 – Loss of VERN (All) B5 – COAS/HUD CAL A6 – Loss of VERN (Tail Only) B6 – A7 – Rendezvous B7 – Rendezvous A8 – Terminal Phase B8 – Terminal Phase A9 – PROX OPS/Flyaround B9 – Flyaround

A10 – Docking B10 – Docking A11 – Auto Reboost B11 – A12 – Mated Stack (Mnvrs, Robotics & Att Hold) B12 – Mated Stack (Undocking and Att Hold) A13 – B13 – Mated Stack (VRCS Deadband Collapse) A14 – Orbiter alone SRMS/OBSS Ops B14 – A15 – B15 –

CNTL ACC – Purpose

0 – Orbiter alone with unloaded RMS 1 – Orbiter alone SRMS/OBSS Ops 2 – Mated - VRCS/ALT, Light Weight Russian Segment 3 – Not used 4 – Mated - VRCS/ALT, Medium Weight Russian Segment 5 – Not used 6 – Mated - VRCS/ALT, Heavy Weight Russian Segment 7 – Not used 8 – Not used 9 – Not used

DAPs for mated operations are based on analysis from GNC, PDRS, C. S. Draper Labs, and ISS Structures

DAP TABLES

FS

3-3 O

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S/135/FIN

UNIV PTG

TGT ID = 1 Orbiting Vehicle TGT ID = 2 Earth Center TGT ID = 3 Earth Target Input LAT (±90) Input LON (±180, + = East) Input ALT (-3444.0 to 20000.0 nm) TGT ID = 4 Sun Center TGT ID = 5 Celestial Target Input RA (0-359.99) Input DEC (±90) TGT ID = 11-110 Nav Stars BODY VECTOR = 1 +X* BODY VECTOR = 2 -X* BODY VECTOR = 3 -Z* BODY VECTOR = 4 -Y Star Tracker* BODY VECTOR = 5 Selectable Input P (0-359.99) Input Y (270-359.99, 0-90) *Input OM → Input OM (0-359.99) MON AXIS = 1 +X MON AXIS = 2 -X

FS

3-4 O

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S/135/FIN

STS-135 DAP A CONFIGURATIONS

STS-135 DAP A1 – DAP A8 CONFIGURATIONS

BOLD/ITALIC indicates change from I-Load.

ITEM # A1 A2 A3 A4 A5 A6 A7 A8PRI

ROT RATE 10 (50) 0.2000 0.4000 0.2000 0.5000 0.2000 0.2000 0.2000 0.0500ATT DB 11 (51) 5.00 1.00 0.30 3.00 5.00 5.00 2.00 2.00RATE DB 12 (52) 0.20 0.20 0.20 0.20 0.20 0.20 0.20 0.20ROT PLS 13 (53) 0.100 0.100 0.100 0.100 0.100 0.100 0.100 0.100COMP 14 (54) .000 .000 .000 .000 .000 .000 .000 .000P OPTION 15 (55) ALL ALL ALL ALL ALL TAIL ALL ALLY OPTION 16 (56) ALL ALL TAIL ALL ALL TAIL ALL ALLTRAN PLS 17 (57) 0.100 0.100 0.100 0.100 0.100 0.100 0.100 0.100

ALT RATE DB 18 (58) 0.200 0.200 0.070 0.200 0.070 0.070 0.100 0.100JET OPT 19 (59) ALL ALL ALL ALL ALL TAIL ALL ALL# JETS 20 (60) 2 2 1 2 1 1 2 2ON TIME 21 (61) 0.08 0.08 0.08 0.08 0.08 0.08 0.08 0.08DELAY 22 (62) 0.00 0.00 0.00 0.00 0.00 0.00 0.00 0.00

VERN ROT RATE 23 (63) 0.2000 0.4000 0.0080 0.2000 0.0500 0.0500 0.0160 0.0500ATT DB 24 (64) 1.000 1.000 0.070 1.000 1.000 1.000 1.000 1.000RATE DB 25 (65) .020 .020 .010 .020 .020 .020 .020 .020ROT PLS 26 (66) 0.010 0.010 0.010 0.010 0.010 0.010 0.010 0.050COMP 27 (67) .000 .000 .000 .000 .000 .000 .000 .000CNTL ACC 28 (68) 0 0 0 0 0 0 0 0PURPOSE NOMINAL PTC GG LOSS OF

VERN (ALL) LOSS OF

VERN (TAIL ONLY)

RNDZ TERMINAL PHASE

FS

3-5 O

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OP

S/135/FIN


BOLD/ITALIC indicates change from I-Load. 1 I-loaded below keyboard limit; do not change 2 CA2 – Light Weight Russian Segment 2 CA4 – Medium Weight Russian Segment 2 CA6 – Heavy Weight Russian Segment 3 Use 1 for OBSS scan and 2 for Orbiter attitude maneuvers

ITEM # A9 A10 A11 A12 A13 A14PRI

ROT RATE 10 (50) 0.1300 0.0500 0.0500 0.0500 0.0500 0.2000ATT DB 11 (51) 2.00 0.60 10.00 5.00 5.00 5.00RATE DB 12 (52) 0.10 0.10 0.20 0.20 0.20 0.20ROT PLS 13 (53) 0.100 0.100 0.100 0.040 0.040 0.100COMP 14 (54) .000 .000 .000 .000 .000 .000P OPTION 15 (55) TAIL TAIL TAIL TAIL TAIL TAILY OPTION 16 (56) TAIL TAIL TAIL TAIL TAIL TAILTRAN PLS 17 (57) 0.050 0.050 0.100 0.010 0.010 0.100

ALT RATE DB 18 (58) 0.100 0.100 0.020 1 0.020 1 0.020 1 0.200JET OPT 19 (59) TAIL TAIL TAIL TAIL TAIL TAIL# JETS 20 (60) 2 2 1 1 1 1(2) 3 ON TIME 21 (61) 0.08 0.08 0.08 0.08 0.08 0.08DELAY 22 (62) 0.00 0.00 5.00 5.00 5.00 6.00

VERN ROT RATE 23 (63) 0.1300 0.0500 0.1000 0.1000 0.1000 0.2000ATT DB 24 (64) 1.000 0.500 5.000 3.000 3.000 3.000RATE DB 25 (65) .020 .020 .050 .020 .020 .200ROT PLS 26 (66) 0.050 0.050 0.010 0.002 0.002 0.010COMP 27 (67) .000 .000 .000 .000 .000 .000CNTL ACC 28 (68) 0 0 6(2,4) 2 6(2,4) 2 6(2,4) 2 1PURPOSE PROX/OPS

FLYAROUND DOCKING AUTO

REBOOST MATED STACK

(MNVRS, ROBO, ATT HOLD)

ORBITERALONE

SRMS/OBSS

FS

3-6 O

RB

OP

S/135/FIN

STS-135 DAP B CONFIGURATIONS

STS-135 DAP B1 – DAP B8 CONFIGURATIONS


ITEM # B1 B2 B3 B4 B5 B6 B7 B8PRI

ROT RATE 30 (50) 0.5000 0.2000 0.2000 0.2000 0.2000 0.5000 0.5000 0.0500ATT DB 31 (51) 3.00 3.00 3.00 0.30 3.00 3.00 2.00 2.00RATE DB 32 (52) 0.20 0.20 0.20 0.20 0.20 0.20 0.20 0.20ROT PLS 33 (53) 0.040 0.040 0.040 0.040 0.040 0.040 0.040 0.040COMP 34 (54) .000 .000 .000 .000 .000 .000 .000 .000P OPTION 35 (55) ALL TAIL ALL TAIL TAIL ALL ALL ALLY OPTION 36 (56) ALL TAIL ALL TAIL TAIL ALL ALL ALLTRAN PLS 37 (57) 0.100 0.020 0.020 0.020 0.020 0.020 0.050 0.050

ALT RATE DB 38 (58) 0.200 0.070 0.070 0.100 0.200 0.200 0.100 0.100JET OPT 39 (59) ALL TAIL ALL ALL ALL ALL ALL ALL# JETS 40 (60) 2 1 1 2 2 2 2 2ON TIME 41 (61) 0.08 0.08 0.08 0.08 0.08 0.08 0.08 0.08DELAY 42 (62) 0.00 0.00 0.00 0.00 0.00 0.00 0.00 0.00

VERN ROT RATE 43 (63) 0.2000 0.2000 0.2000 0.0080 0.0160 0.2000 0.2000 0.0500ATT DB 44 (64) 1.000 1.000 1.000 0.100 0.033 1.000 1.000 1.000RATE DB 45 (65) .020 .020 .020 .010 .020 .020 .020 .020ROT PLS 46 (66) 0.002 0.002 0.002 0.002 0.002 0.002 0.002 0.020COMP 47 (67) .000 .000 .000 .000 .000 .000 .000 .000CNTL ACC 48 (68) 0 0 0 0 0 0 0 0PURPOSE OMS & RCS

BURNS (ORB OPS)

LOSS OF VERN

(TAIL ONLY)

LOSS OF VERN (ALL)

COAS/HUD CAL

RNDZ TERMINAL PHASE

FS

3-7 O

RB

OP

S/135/FIN


BOLD/ITALIC indicates change from I-Load. 1 I-loaded below keyboard limit; do not change 2 CA2 – Light Weight Russian Segment 2 CA4 – Medium Weight Russian Segment 2 CA6 – Heavy Weight Russian Segment

ITEM # B9 B10 B12 B13 PRI

ROT RATE 30 (50) 0.1300 0.0500 0.0100 1 0.0100 1 ATT DB 31 (51) 2.00 0.60 1.00 1.00 RATE DB 32 (52) 0.10 0.10 0.20 0.20 ROT PLS 33 (53) 0.040 0.040 0.040 0.040 COMP 34 (54) .000 .000 .000 .000 P OPTION 35 (55) TAIL TAIL TAIL TAIL Y OPTION 36 (56) TAIL TAIL TAIL TAIL TRAN PLS 37 (57) 0.010 0.010 0.010 0.010

ALT RATE DB 38 (58) 0.100 0.100 0.020 1 0.020 1 JET OPT 39 (59) TAIL TAIL TAIL TAIL # JETS 40 (60) 2 2 1 1 ON TIME 41 (61) 0.08 0.08 0.08 0.08 DELAY 42 (62) 10.00 0.00 5.00 5.00

VERN ROT RATE 43 (63) 0.1300 0.0500 0.0100 0.0100 ATT DB 44 (64) 1.000 0.500 1.000 0.100 RATE DB 45 (65) .020 .020 .020 .020 ROT PLS 46 (66) 0.020 0.020 0.002 0.002 COMP 47 (67) .000 .000 .000 .000 CNTL ACC 48 (68) 0 0 6(2,4) 2 6(2,4) 2 PURPOSE PROXOPS/

FLYAROUND DOCKING MATED

ATT HOLD (VRCS & ALT)

MATED VRCS DB COLLAPSE


REBOOST/DAP

AUTO REBOOST ........................................................... FS 4-2 AUTO REBOOST ATTITUDE REFERENCE ................. FS 4-4 DOCKED DAP REFERENCE ........................................ FS 4-5 RATE DAMPING ............................................................ FS 4-5 ROBOTICS ATTITUDE MAINTENANCE ....................... FS 4-6

REB

OO

ST/

DA

P


AUTO REBOOST

NOTE Allow 5 min between establishing reboost attitude and reboost start time for DAP accelerations to converge

1. If PRCS required: O14:F, RJDA 1A L2/R2 DRIVER – OFF O15:F, RJD MANF L5/F5/R5 DRIVER – OFF O16:F Pri RJD LOGIC (eight) – ON

√MCC for GO to power up Pri Drivers RJD MANF L5/F5/R5 DRIVER – ON Pri RJD DRIVER (eight) – ON

2. Select Reboost Configuration

GNC 20 DAP CONFIGREBOOST CFG – ITEM 8 +_ EXEC INTVL – ITEM 9 +_ _ _._ _ EXEC

3. Set up Future Reboost

GNC UNIV PTGDURATION – ITEM 27 +_ _+_ _+_ _._ _ EXEC START TIME – ITEM 1 +_ _ _+_ _+_ _+_ _ EXEC

RBST – ITEM 25 EXEC (FUT-*) 4. Select appropriate Reboost Rotation DAP

When in attitude and prior to START TIME, C3 DAP: A11/AUTO/VERN(ALT)

If using Config 4(1):

GNC 20 DAP CONFIGDisable X JETS ROT – ITEM 7 EXEC (no *)

REB

OO

ST/

DA

P

Cont next page


NOTE Reboost can be aborted with an ITEM 26 on UNIV PTG or by selecting FREE on the DAP

5. Post Reboost Configuration

If using Config 4(1):

GNC 20 DAP CONFIGEnable X JETS ROT – ITEM 7 EXEC (*)

Return to FLIGHT PLAN Attitude

C3 DAP: as reqd O14, Pri RJD LOGIC,DRIVER (sixteen) – as reqd O15, O16


AUTO REBOOST ATTITUDE REFERENCE

ALT & VRCS ATTITUDE HOLD CONFIGURATIONS:

Configurations 1 and 4 use ALT PRCS (Pitch, X=4°) Configuration 2 is for Shuttle only - Do Not Use While Docked Configuration 3 uses VRCS (Pitch, X=4°)


DOCKED DAP REFERENCE

NOTE Shuttle mated attitude control is not certified when the Shuttle Airlock is depressurized (<3.45 psia)

Mated Attitude Hold and Maneuvers

(VERN or ALT) Mated Attitude Hold

(VERN or ALT)

A12 B12 ALT not certified for loaded RMS operations CNTL ACC selection depends on the weight of the Russian Segment due to visiting vehicle configurations as described below:

SM AFT EMPTY

SM AFT OCCUPIED

MRM2 AND/OR DC1 EMPTY

LIGHT (CNTL ACC 2)

MEDIUM (CNTL ACC 4)

MRM2 AND DC1 OCCUPIED

MEDIUM (CNTL ACC 4)

HEAVY (CNTL ACC 6)

RATE DAMPING

DAP: LVLH(INRTL) - Dependent on desired attitude hold Monitor Jet Activity Light:

For continuous Jet Activity > 6 min: DAP: FREE then restart this procedure

If Jet Activity Stopped for > 5 sec for VERN (15 sec for ALT) DAP: FREE > 2 sec DAP: AUTO >>

ORB OPS/135/FIN 1


ROBOTICS ATTITUDE MAINTENANCE

1. DAP: LVLH 2. When no jet activity for >5 sec (Rates Damped): DAP: FREE > 2 sec DAP: AUTO 3. If continuing with Loaded Robotics Ops: When in attitude and no jet activity for >5 sec: DAP: FREE


OIU PROCEDURES

OIU ACTIVATION .......................................................... FS 5-2 OIU DEACTIVATION ..................................................... FS 5-2

OIU


OIU ACTIVATION

NOTE √MCC that steps 1 and 2 may not be reqd

1. Load PCMMU/PDI (config 760) for OIU 2. Power on PSP 1(2) A1L √S-BD PL CNTL – CMD

PWR SYS – 1(2) √SEL – PSP √PSP CMD OUTPUT – PL UMB CNTL – PNL,CMD

SM 62 PCMMU/PL COMM

I/O RESET PSP 1(2) – ITEM 6(7) EXEC (*) 3. Power on OIU 1(2) SSP1 OIU PWR – OIU 1(2) ON

√tb – UP(DN) OIU DEACTIVATION

NOTE √MCC for OIU ops complete

1. Possible ‘S62 PDI DECOM FAIL’ msg SSP1 OIU PWR – OFF

√tb – bp 2. MCC will config PCMMU and PDI as reqd

OIU


SHORT DURATION BIOASTRONAUTICS INVESTIGATION (SDBI)

SDBI 1634, SLEEP-WAKE ACTIGRAPHY .................... FS 6-2 DON ACTIWATCH .................................................... FS 6-2 DOFF ACTIWATCH .................................................. FS 6-2

SDB

I


SDBI 1634, SLEEP-WAKE ACTIGRAPHY

A. DON ACTIWATCH (ASAP after entry into orbit) MF28K 1. Unstow: Actiwatch

Unstow: SLEEP LOGBOOK

NOTE Actiwatch should be worn on top of non-dominant wrist outside of clothing. Face of Actiwatch should remain uncovered at all times. If necessary to remove Actiwatch, record doff/don time in SLEEP LOGBOOK

2. Don Actiwatch on non-dominant arm and wear

continuously throughout mission 3. Deploy SLEEP LOGBOOK and record required

information daily (within 15 min after waking)

B. DOFF ACTIWATCH

NOTE If mission length extended, continue to wear Actiwatch and complete SLEEP LOGBOOK as timeline permits

On final day of orbit:

MF28K 1. Remove Actiwatch, stow in locker 2. Recover SLEEP LOGBOOK, stow in locker

SDB

I

ORB OPS/135/FIN 1


WING LEADING EDGE SENSORS (WLES) PROCEDURES

WLES ACTIVATION AND CHECKOUT ......................... FS 7-2 WLES DEACTIVATION AND TEARDOWN ................... FS 7-10 WLES LAPTOP RECEIVER UNIT (LRU) R&R .............. FS 7-12 WLES CABIN RELAY UNIT R&R .................................. FS 7-14 CONFIGURE WLES DATA FILE BACKUP PATH ......... FS 7-16 PREP WLES LAPTOPS FOR TRANSFER .................... FS 7-17 WLES RNDZ TOOLS CHECKOUT PREP ..................... FS 7-18 WLES DOCK/UNDOCK RECOVERY ............................ FS 7-18 DISABLE WLES FILE BACKUP .................................... FS 7-19 ENABLE WLES FILE BACKUP ..................................... FS 7-19 LRU TROUBLESHOOTING ........................................... FS 7-20

WLE

SE

NSO

RS


WLES ACTIVATION AND CHECKOUT

1. UNSTOW EQUIPMENT NOTE

A31p laptops may already be unstowed as part of orbiter laptop network setup

Unstow: MA9J Laptop Receiver Units (2)

Cabin Relay Units (2): CRU A (S/N 2432) CRU B (S/N 2496)

ML60E STS6 A31p laptop (WLES) STS5 A31p laptop (RPOP2)

2. SETUP WLES RELAY UNITS

CAUTION Cross-connecting CRU A to MICRO WIS SYSTEM B (and vice versa) will prevent WLES ops, though step 8 would still show good comm

NOTE

Green patch on Cabin Relay Unit is antenna and must face into cabin

A6 Unstow coiled WLE SYSTEM A cable A13 Connect plug PNL A13 SYSTEM A to jack MICRO

WIS SYSTEM A J7 (see fig 7-1) CRU A Connect plug CABIN RELAY UNIT (P1 SYSTEM A)

to J1 on CRU S/N 2432 STBD Secure CRU A to STBD side of aft cabin with Velcro OVHD (see fig 7-2) A9 Unstow coiled WLE SYSTEM B cable A13 Connect plug PNL A13 SYSTEM B to jack MICRO

WIS SYSTEM B J8 (see fig 7-1) CRU B Connect plug CABIN RELAY UNIT (P1 SYSTEM B)

to J1 on CRU S/N 2496 PORT Secure CRU B to PORT side of aft cabin with Velcro OVHD (see fig 7-3)

WLE

SE

NSO

RS



Figure 7-1.- A13 panel.

Cont next page


Figure 7-2.- Aft STBD location.

Figure 7-3.- Aft PORT location.

Cont next page


NOTE Laptops may be powered or unpowered. Laptops may be connected to network or standalone

3. SETUP PRIME WLES LAPTOP A31p Secure Laptop Receiver Unit to A31p with Velcro

(see fig 7-4) Connect Laptop Receiver Unit to A31p Serial port using thumbscrews (see fig 7-5)

Verify line of sight between Laptop Receiver Unit and both CRUs

Verify 5-in minimum distance between Laptop Receiver Unit and both CRUs

4. SETUP BACKUP WLES LAPTOP

NOTE Single laptop ops are preferred over delays in activation. If problems with Backup Laptop occur, skip step 4

Secure Laptop Receiver Unit to A31p with Velcro (see fig 7-4)

Connect Laptop Receiver Unit to A31p Serial port using thumbscrews (see fig 7-5)

Verify line of sight between Laptop Receiver Unit and both CRUs

Verify 5-in minimum distance between Laptop Receiver Unit and both CRUs

Figure 7-4.- Laptop Receiver Unit.

Cont next page


Serial Port

Figure 7-5.- A31p ports.

5. LAUNCH WLES SOFTWARE

Perform for both laptops: If laptops are off, A31p pwr – On Double click the time in system tray (lower-right corner)

‘Date and Time Properties’ ‘Time Zone’ Time zone – (GMT) Greenwich Mean Time Click ‘OK’ Double click ‘Shuttle Apps’>‘WLES’>‘WLES’ ‘Backup Mode Selection’ If setting up one A31p, select ‘Standard’

If setting up two A31p laptops:

For prime laptop, select ‘Primary’ For backup laptop, select ‘Secondary’

If ‘EWBMTAU-WLEFlight’ appears with message ‘Run the current command: XXXX_AA_BB_SNYYYY.xml?’:

Click ‘Yes’ NOTE

The secondary laptop lid may be closed at this time, if no longer needed for other applications. The laptops are configured so that they do not enter ‘standby’ or ‘hibernate’ mode when the lids are closed. However, due to cooling concerns, fully closing the lid is not recommended

Cont next page


6. VERIFY LRU INSTALLATION A31p Use prime WLES laptop

‘Enhanced Wideband MicroTAU – WLEFlight 3.0’ Click ‘System Settings’ (left side of display) ‘Communications Settings’

√RF Receiver Port: ‘COM 1’ Click ‘Query Receiver’ Verify ‘Receiver found on COM1’ message appears

* ********

If ‘Query Receiver’ fails: Reseat LRU Reboot prime WLES laptop Double click ‘Shuttle Apps’>‘WLES’> ‘WLES’

Select ‘Primary’ Repeat step 6

If no Joy, perform WLES LRU R&R, steps 1-4, 6, then:

* ********

7. VERIFY DATA FILE BACKUP

Use prime WLES laptop Verify ‘Backup Directory:’ set to: ‘S:\Program Files\Invocon\EWBMTAU-WLEFlight’

* ************

If ‘Backup Directory’ not set as above: ‘System Settings’ ‘Directories’ At the line ‘Backup Directory:’ click ‘Browse…’ (right side of display)

‘Browse for Folder’ Navigate to WLES folder on RPOP2:

‘My Computer’>‘C on RPOP2 (S:)’> ‘Program Files’>‘Invocon’> ‘EWBMTAU-WLEFlight’

Click ‘OK’

* ************

Verify ‘Backup Interval’ set to ‘30 minutes’

Cont next page


8. VERIFY COMM WITH RELAY UNITS Use prime WLES laptop

‘Main’ Click ‘Unit List’ (left side of display)

NOTE

Each Cabin Relay Unit is identified with a unique serial number; this number appears as ‘Unit ID’ in the software

√Cabin Relay Units Unit ID 2432 and 2496 present on

display in first column; scroll down as necessary For each Cabin Relay Unit: √Unit ID present √Type: ‘Relay-GL’ √Last Update: time is updating (every 5 to 15 sec)

* *****

If one CRU time does not update: Perform WLES CABIN RELAY UNIT R&R,

steps 1 thru 3, then: Go to step 9 If neither CRU time updates after 2 min, contact MCC-H

* *****

√Via: ‘RF’ √Mode: ‘Idle’

9. INITIATE COMMANDING

Double click ‘Shuttle Apps’>‘WLES’>‘WLES Data Folder’

Double click ‘Shuttle Apps’>‘WLES’>‘WLES Cmd Folder’

Cont next page


NOTE Deleting ‘BLOCK.xml’ file initiates command execution. Command files disappear from this folder as they are executed. Files appearing in the ‘Data’ folder verifies two-way communication with the Sensor Units in the orbiter wing

‘Command’ Delete file labeled ‘BLOCK.xml’ At prompt “Are you sure you want to send ‘Block.xml’ to the Recycle Bin?”, click ‘Yes’

Wait 1 minute Verify the first data file appears in the ‘Data’ folder

Close ‘Command’ and ‘Data’ folders

10. REPORT WLES STATUS

Notify MCC-H: “WLES setup complete”

If reporting a failed and replaced CRU, include: Failed CRU S/N

NOTE

The laptop lid may be closed at this time, if no longer needed for other applications. The laptops are configured so that they do not enter ‘standby’ or ‘hibernate’ mode when the lids are closed. However, due to cooling concerns, fully closing the lid is not recommended


WLES DEACTIVATION AND TEARDOWN 1. DEACTIVATE WLES LAPTOP

NOTE MCC will configure WLES for entry by setting all sensor units to idle mode

On MCC GO: A31p ‘Enhanced Wideband MicroTAU – WLEFlight 3.0’

For each WLES A31p: Click ‘Exit’ At prompt ‘Are you sure you want to exit?’ click ‘Yes’

Click ‘Start’>‘Turn Off Computer…’>‘Turn Off’ Disconnect Laptop Receiver Unit from A31p Serial port

Remove Laptop Receiver Unit from Velcro on A31p

2. REMOVE WLES RELAY UNITS Remove Cabin Relay Units (2) from aft cabin (see figs 7-6 and 7-7)

Disconnect Cabin Relay Units from pre-routed cables

Disconnect and coil cables, stow in launch location

Figure 7-6.- Aft STBD location.

Cont next page


Figure 7-7.- Aft PORT location. 3. STOW EQUIPMENT MA9J Stow:

Laptop Receiver Units (2) Cabin Relay Units (2)

Notify MCC-H: “WLES Teardown Complete”

ORB OPS/135/FIN 1


WLES LAPTOP RECEIVER UNIT (LRU) R&R

1. DISCONNECT BACKUP LRU FROM LAPTOP A31p ‘Enhanced Wideband MicroTAU – WLEFlight 3.0’

Click ‘Exit’ At prompt ‘Are you sure you want to exit?’ click ‘Yes’

Disconnect Backup LRU from Backup A31p Serial port (see fig 7-8)

Remove Backup LRU from Velcro on Backup A31p (see fig 7-9)

Serial Port

Figure 7-8.- A31p ports.

Figure 7-9.- Laptop Receiver Unit. 2. DISCONNECT PRIME LRU FROM LAPTOP

Disconnect Prime LRU from Prime A31p Serial port (see fig 7-8)

Remove LRU from Velcro on A31p

Cont next page


3. CONNECT BACKUP LRU Connect Backup LRU to Prime WLES A31p Serial port

Secure LRU to A31p with Velcro

4. VERIFY LRU INSTALLATION A31p Use prime WLES laptop

‘Enhanced Wideband MicroTAU – WLEFlight 3.0’ Click ‘System Settings’ (left side of display)

‘Communications Settings’

RF Receiver Port: ‘COM 1’

Click ‘Query Receiver’ Verify ‘Receiver found on COM1’ message appears

5. VERIFY COMM WITH RELAY UNITS

Click ‘Unit List’ (left side of display) Cabin Relay Units Unit ID 2432 and 2496 present on

display in first column; scroll down as necessary For each Cabin Relay Unit: Unit ID present Type: ‘Relay-GL’ Last Update: time is updating (every 5 to 15 sec) Via: ‘RF’ Mode: ‘Idle’

If no time updates after 2 min, contact MCC-H

6. STOW EQUIPMENT

Notify MCC-H: “WLES LRU R&R complete”, mark failed LRU as ‘failed’

MA9J Stow:

Prime (failed) LRU

ORB OPS/135/FIN 1


WLES CABIN RELAY UNIT R&R

1. DISCONNECT FAILED CRU AND STOW OVHD Disconnect WLE SYSTEM cable from J1 connector

on failed CRU Mark failed CRU as ‘failed’ and stow in ML60E

2. SETUP SPARE WLES RELAY UNIT

MA9J Unstow CRU SPARE (S/N 2304)

WLE SYSTEM cable Connect plug CABIN RELAY UNIT A or B to J1 on CRU S/N 2304

OVHD Secure CRU SPARE to the aft cabin with Velcro

3. VERIFY COMM WITH SPARE RELAY UNIT A31p Use prime WLES laptop


NOTE

Each Cabin Relay Unit is identified with a unique serial number; this number appears as ‘Unit ID’ in the software

Cabin Relay Unit Unit ID 2304 present on display in

first column; scroll down as necessary Cabin Relay Unit: Unit ID present Type: ‘Relay-GL’ Last Update: time is updating (every 5 to 15 sec) Via: ‘RF’ Mode: ‘Idle’

NOTE

Loss of redundant relay path until the config file is updated by the ground



4. EXIT WLES SOFTWARE ON BOTH LAPTOPS

On MCC GO: A31p On both Prime and Backup WLES laptops:

‘Enhanced Wideband MicroTAU – WLEFlight 3.0’ Click ‘Exit’ (upper right side of display)

‘EWBMTAU – WLEFlight’ ‘Are you sure you want to exit?’, click ‘Yes’

Notify MCC-H when complete

NOTE

OCA will replace the config files on both laptops

5. LAUNCH WLES SOFTWARE

On MCC GO: A31p On both Prime and Backup WLES laptops:

Double click ‘Shuttle Apps’>‘WLES’>‘WLES’

‘Backup Mode Selection’ If setting up one A31p, select ‘Standard’

If setting up two A31p laptops:

For prime laptop, select ‘Primary’ For backup laptop, select ‘Secondary’

If ‘EWBMTAU-WLEFlight’ window appears with message ‘Run the current command: XXXX_AA_BB_SNYYYY.xml?’:

Click ‘Yes’

6. REVERIFY COMM WITH SPARE RELAY UNIT Repeat step 3

7. REPORT WLES STATUS

Notify MCC-H: “WLES CRU R&R complete”


CONFIGURE WLES DATA FILE BACKUP PATH

NOTE MCC will identify new backup WLES laptop to be used in place of RPOP2 (S:)

A31p Use prime WLES laptop


‘Directories’ At the line ‘Backup Directory:’ click ‘Browse…’ (right side of display)

‘Browse for Folder’ Navigate to WLES folder on RPOP2:

‘My Computer’>‘C on RPOP2 (S:)’>‘Program Files’>‘Invocon’>‘EWBMTAU-WLEFlight’

Click ‘OK’

Verify ‘Backup Directory:’ set to: ‘S:\Program Files\Invocon\EWBMTAU-WLEFlight’


Click ‘Unit List’ (left side of display)


PREP WLES LAPTOPS FOR TRANSFER

1. DEACTIVATE WLES LAPTOP(S) A31p ‘Enhanced Wideband MicroTAU – WLEFlight 3.0’

For each WLES A31p to be transferred: Click ‘Exit’ At prompt ‘Are you sure you want to exit?’ click ‘Yes’

Click ‘Start’>‘Turn Off Computer…’>‘Turn Off’ Disconnect Laptop Receiver Unit from A31p Serial port

Remove Laptop Receiver Unit from Velcro on A31p

2. SET UP NEW WLES LAPTOPS √MCC-H for which laptop to use

If Prime Laptop being transferred: Perform WLES ACTIVATION AND CHECKOUT, steps 3, 5 thru 8, then:

If Backup Laptop being transferred:

Perform WLES ACTIVATION AND CHECKOUT, steps 4 and 5, then:

Notify MCC-H: “PREP WLES LAPTOPS FOR TRANSFER complete”


WLES RNDZ TOOLS CHECKOUT PREP

1. DEACTIVATE BACKUP WLES LAPTOP A31p On backup WLES laptop:

‘Enhanced Wideband MicroTAU – WLEFlight 3.0’ Click ‘Exit’ At prompt ‘Are you sure you want to exit?’ click ‘Yes’

Disconnect Laptop Receiver Unit from A31p Serial port

Leave attached to laptop with Velcro on A31p 2. DEACTIVATE WLES FILE BACKUP

On prime WLES laptop: ‘Enhanced Wideband MicroTAU – WLEFlight 3.0’ Click ‘System Settings’ (left side of display)

‘Backup Mode Selection’ Click ‘Standard’ Click ‘Unit List’ (left side of display)

WLES DOCK/UNDOCK RECOVERY

1. RECOVER BACKUP WLES LAPTOP A31p On backup WLES laptop:

Connect Laptop Receiver Unit to A31p Serial port If laptop is off:

A31p pwr – On At prompt select option 1 to start WLES

If laptop is on: Double click ‘Shuttle Apps’>‘WLES’>‘WLES’ ‘Backup Mode Selection’ Click ‘Secondary’

2. REACTIVATE WLES FILE BACKUP

On prime WLES laptop: ‘Enhanced Wideband MicroTAU – WLEFlight 3.0’ Click ‘System Settings’ (left side of display) ‘Backup Mode Selection’ Click ‘Primary’ Click ‘Unit List’ (left side of display)


DISABLE WLES FILE BACKUP (SWITCH TO STANDARD MODE)

A31p On prime WLES laptop: ‘Enhanced Wideband MicroTAU – WLEFlight 3.0’ Click ‘System Settings’ (left side of display)

‘Backup Mode Selection’ Click ‘Standard’ Click ‘Unit List’ (left side of display)

ENABLE WLES FILE BACKUP (SWITCH TO PRIMARY MODE)

A31p On prime WLES laptop: ‘Enhanced Wideband MicroTAU – WLEFlight 3.0’ Click ‘System Settings’ (left side of display)

‘Backup Mode Selection’ Click ‘Primary’ Click ‘Unit List’ (left side of display)


LRU TROUBLESHOOTING

NOTE This procedure requires 30 min crew time or 15 min if the ground can verify good COM 1

1. VERIFY LINE OF SIGHT

Verify unobstructed line of sight between LRU and both CRUs

Verify 5-in minimum distance between LRU and both CRUs

2. VERIFY COMM WITH RELAY UNITS A31p Use prime WLES laptop

‘Enhanced Wideband MicroTAU – WLEFlight 3.0’ ‘Main’ Click ‘Unit List’ (left side of display)


display in first column; scroll down as necessary For each Cabin Relay Unit: √Unit ID present √Type: ‘Relay-GL’ √Last Update: time is updating (every 5 to 15 sec) √Via: ‘RF’ √Mode: ‘Idle’

If both times updating:

Notify MCC: “Line of sight problem” >>

If both times not updating: Notify MCC and proceed to step 3

3. RESEAT LRU AND RESTART LAPTOP

Completely disconnect and then reconnect LRU from serial port on prime WLES laptop

If other applications are running on prime WLES laptop, √MCC

Cont next page



‘EWBMTAU - WLEFlight’ ‘Are you sure you want to exit?’, click ‘Yes’

Reboot prime WLES laptop

Click ‘1’ to launch WLES Software

‘Backup Mode Selection’ Select ‘Primary’




√RF Receiver Port: ‘COM 1’


If ‘Timeout exceeded…’ message appears:

Notify MCC and proceed to step 5




Cont next page


If both times updating: Notify MCC: “Computer problem/bad LRU connection” >>

If both times not updating:

Notify MCC and proceed to step 5 5. REPLACE FAILED LRU

Perform WLES LAPTOP RECEIVER UNIT (LRU) R&R, then:

If both times updating in LRU R&R step 5:

Notify MCC: “LRU Failure” >>

If both times not updating in LRU R&R step 5: Notify MCC and proceed to step 6

6. EXIT SOFTWARE ON PRIME WLES LAPTOP

Use prime WLES laptop


‘EWBMTAU – WLEFlight’ ‘Are you sure you want to exit?’, click ‘Yes’

7. RETURN BACKUP LRU TO BACKUP WLES

LAPTOP Disconnect Backup LRU from Prime A31p Serial port

Remove Backup LRU from Velcro on Prime A31p Connect Backup LRU to Backup A31p Serial port Secure Backup LRU to Backup A31P with Velcro Verify unobstructed line of sight between LRU and both CRUs

Verify 5-in minimum distance between LRU and both CRUs

Cont next page


8. CONFIGURE BACKUP WLES LAPTOP AS NEW PRIME LAPTOP

Use backup WLES laptop

Double click ‘Shuttle Apps’>‘WLES’>‘WLES’ ‘Backup Mode Selection’ Click ‘Primary’


Use backup WLES laptop



√RF Receiver Port: ‘COM 1’





If both times updating:

Notify MCC: “Serial port hardware failure on prime WLES laptop”

Go to step 10

If both times not updating: √MCC >>

Cont next page


10. CONFIGURE NEW BACKUP PATH Use backup WLES laptop

‘Enhanced Wideband MicroTAU – WLEFlight 3.0’

‘System Settings’ ‘Directories’ At the line ‘Backup Directory:’ click ‘Browse…’ (right side of display)

‘Browse for Folder’ Navigate to WLES folder on WLES:

‘My Computer’>’C on WLES (V:)’>‘Program Files’>’Invocon’>‘EWBMTAU-WLEFlight’

Click ‘OK’

Verify ‘Backup Directory:’ set to: ‘V:\Program Files\Invocon\EWBMTAU-WLEFlight’


Click ‘Unit List’ (left side of display)

Notify MCC: “LRU Troubleshooting Complete”

MA9J Stow:

Prime LRU

ORB OPS/135/FIN 1


PAYLOADS OF OPPORTUNITY

MAUI PRCS AND VRCS PROCEDURE ........................ FS 8-2 MAUI VRCS ONLY PROCEDURE ................................ FS 8-6 MAUI PRCS ONLY PROCEDURE ................................ FS 8-10 RAMBO-2 PROCEDURE ............................................... FS 8-14

P/L

OF

OPP


MAUI PRCS AND VRCS PROCEDURE

-15:00 1. MANEUVER TO START ATTITUDE or earlier (BIASED +ZLV +YVV)

NOTE External lights should remain OFF from 15 minutes before, until 5 minutes after the MAUI burn

A7U √PL BAY FLOOD (all) – OFF √ILLUMINATORS (all) – OFF

Deploy MAUI PRCS AND VRCS – RCS FIRING SEQUENCE (Cue Card)

GNC 20 DAP CONFIG

√DAP A1, B1 loaded

UNIV PTGTGT ID – ITEM 8 +2 EXEC BODY VECT – ITEM 14 +5 EXEC P – ITEM 15 +2 7 0 EXEC Y – ITEM 16 +3 5 0 EXEC OM – ITEM 17 +2 7 0 EXEC TRK – ITEM 19 EXEC (CUR - *)

2. INITIATE TIMER

√MCC for start time

GNC 2 TIMESet count down/count up timer per MCC

√MET – ITEM 2 EXEC (*) CRT TIMER COUNT TO – ITEM 17 +_ _ +_ _ +_ _

EXEC 3. SETUP

O14:E, cb DDU L (two) – cl O15:E O14:F, Pri RJD LOGIC,DRIVER (sixteen) – ON O15:F, O16:F

Cont next page

P/L

OF

OPP


GNC 20 DAP CONFIGDAP A PRI P OPTION – ITEM 15 EXEC (NOSE) DAP A PRI TRAN PLS – ITEM 17 +0.7 3 EXEC DAP A VERN ROT PLS – ITEM 26 +0.1 5 3 EXEC

C3 √DAP: A/AUTO/VERN

√DAP TRANS: PULSE/PULSE/PULSE

4. VERIFY ATTITUDE -05:00 Verify in attitude

DAP ROT: PULSE/PULSE/PULSE

NOTE For the following RCS firing sequence (step 5):

A. Expect total orbiter body rates

(RSS) to exceed 1 deg/sec

B. Possible loss of comm due to orbiter body rates and attitude excursions

C. For any jet fail OFF, continue with

firing sequence

D. Requirement is for a particular jet group, not a specific jet

E. The table in step 5 is also provided

as a cue card

Cont next page


5. MAUI PRCS AND VRCS - RCS FIRING SEQUENCE

NOTE

Use the table below or the cue card

Reminder: All inputs are momentary

Timer Jets Fired CDR PLT-03:00 √Body rates:

+0.047 ≤ roll ≤ +0.087 -0.020 ≤ pitch ≤ +0.020 -0.020 ≤ yaw ≤ +0.020

DAP: FREE DAP: A/PRI Inform PLT “GO” for jet deselects

Configure initial setup GNC 23 RCS

Left RCS page – ITEM 2 EXEC On CDR “GO”, proceed

NOTE Expect DAP RECONF msgs in following actions

Deselect jets: JET DES L5L – ITEM 37 EXEC (*) Right RCS page – ITEM 3 EXEC JET DES R5D – ITEM 39 EXEC (*) Forward RCS page – ITEM 1 EXEC JET DES F5L – ITEM 37 EXEC (*)

-00:30 FLT CNTLR PWR – ON 00:00 RXA, LXA THC +X (in) (3 sec firing) 00:15 FXL, LXL THC +Y (right) (3 sec firing) 00:30 FXR, RXR THC -Y (left) (3 sec firing) 00:35 DAP: VERN 00:45 R5R RHC +yaw (10 sec firing)

Do not exceed soft stop

01:05 L5D RHC -pitch (12 sec firing) Do not exceed soft stop

01:25 F5R RHC +pitch (12 sec firing) Do not exceed soft stop

FLT CNTLR PWR – OFF Return to MAUI PRCS AND VRCS PROCEDURE, step 6, (ORB OPS FS, P/L OF OPP)

Cont next page


6. CLEANUP F6 √FLT CNTLR PWR – OFF

GNC 23 RCS√Forward RCS page – ITEM 1 EXEC

Reselect Jets: JET DES F5L – ITEM 37 EXEC (no *)

Left RCS page – ITEM 2 EXEC JET DES L5L – ITEM 37 EXEC (no *)

Right RCS page – ITEM 3 EXEC JET DES R5D – ITEM 39 EXEC (no *)

GNC 20 DAP CONFIG

DAP A1 – ITEM 1 +1 EXEC 7. SNAP LVLH ATTITUDE AND NULL RATES

When time ≥ +03:30: DAP: A/PRI DAP: LVLH

When rates stable:

DAP: VERN

Return to FLT PLN attitude 8. RECONFIGURE TO GROUP B POWERDOWN

√MCC O14:E, cb DDU L (two) – op O15:E O14:F, Pri RJD LOGIC,DRIVER (sixteen) – OFF O15:F, RJDA 1A L2/R2 MANF DRIVER – ON O16:F


MAUI VRCS ONLY PROCEDURE

-15:00 1. MANEUVER TO START ATTITUDE or earlier (BIASED -XLV +ZVV)



Deploy MAUI VRCS ONLY FIRING SEQUENCE (Cue Card)

GNC 20 DAP CONFIG


UNIV PTGTGT ID – ITEM 8 +2 EXEC BODY VECT – ITEM 14 +5 EXEC P – ITEM 15 +1 8 0 EXEC Y – ITEM 16 +0 EXEC OM – ITEM 17 +0 EXEC TRK – ITEM 19 EXEC (CUR - *)

2. INITIATE TIMER




EXEC 3. SETUP

O14:E, cb DDU L (two) – cl O15:E

GNC 20 DAP CONFIGDAP A VERN ROT PLS – ITEM 26 +0.1 5 3 EXEC


Cont next page



DAP ROT: PULSE/PULSE/PULSE NOTE

For the following VRCS firing sequence (step 5):

A. Possible loss of comm due to orbiter body rates and attitude excursions

B. For any jet fail OFF, continue with firing sequence

C. The table in step 5 is also provided as a cue card

5. VRCS ONLY FIRING SEQUENCE

NOTE Use the table below or the cue card

Reminder: All inputs are momentary Timer Jets Fired CDR PLT

-02:00 √Body rates: -0.020 ≤ roll ≤ +0.020 -0.087 ≤ pitch ≤ -0.047 -0.020 ≤ yaw ≤ +0.020

DAP: FREE √DAP: VERN Inform PLT “GO” for jet deselects


Left RCS page – ITEM 2 EXEC (*) On CDR “GO”, proceed


Deselect jets: JET DES L5L – ITEM 37 EXEC (*) Right RCS page – ITEM 3 EXEC (*) JET DES R5D – ITEM 39 EXEC (*) Forward RCS page – ITEM 1 EXEC (*)

JET DES F5L – ITEM 37 EXEC (*) -00:30 FLT CNTLR PWR – ON 00:00 R5R RHC +yaw (10 sec firing)




FLT CNTLR PWR – OFF Return to MAUI VRCS ONLY PROCEDURE, step 6, (ORB OPS FS, P/L OF OPP)

Cont next page Cont next page




Reselect Jets: JET DES F5L – ITEM 37 EXEC (no *)

Left RCS page – ITEM 2 EXEC JET DES L5L – ITEM 37 EXEC (no *)

Right RCS page – ITEM 3 EXEC JET DES R5D – ITEM 39 EXEC (no *)

GNC 20 DAP CONFIG


When time ≥ +02:00: DAP: LVLH

Return to FLT PLN attitude

8. RECONFIGURE TO GROUP B POWERDOWN

√MCC O14:E, cb DDU L (two) – op O15:E


MAUI PRCS ONLY PROCEDURE

-15:00 1. MANEUVER TO START ATTITUDE or earlier (BIASED +ZLV +YVV)



Deploy MAUI PRCS ONLY FIRING SEQUENCE (Cue Card)

GNC 20 DAP CONFIG


UNIV PTGTGT ID – ITEM 8 +2 EXEC BODY VECT – ITEM 14 +5 EXEC P – ITEM 15 +2 7 0 EXEC Y – ITEM 16 +3 5 0 EXEC OM – ITEM 17 +2 7 0 EXEC TRK – ITEM 19 EXEC (CUR - *)

2. INITIATE TIMER




EXEC 3. SETUP

O14:E, cb DDU L (two) – cl O15:E O14:F, Pri RJD LOGIC,DRIVER (sixteen) – ON O15:F, O16:F

Cont next page


GNC 20 DAP CONFIGDAP A PRI P OPTION – ITEM 15 EXEC (NOSE) DAP A PRI ROT PLS – ITEM 13 +1.0 0 0 EXEC DAP A PRI TRAN PLS – ITEM 17 +0.7 8 EXEC

GNC 23 RCS

Deselect Jets: Forward RCS page – ITEM 1 EXEC JET DES F1D – ITEM 23 EXEC (*) F2D – ITEM 27 EXEC (*)


√DAP TRANS: PULSE/PULSE/PULSE


NOTE For the following PRCS firing sequence (step 5):

A. Expect total orbiter body rates

(RSS) to exceed 1 deg/sec

B. Possible loss of comm due to orbiter body rates and attitude excursions

C. For any jet fail OFF, continue with

firing sequence

D. Requirement is for a particular jet group, not a specific jet

E. The table in step 5 is also provided

as a cue card

Cont next page


5. PRCS FIRING SEQUENCE

NOTE Use the table below or the cue card

Reminder: all inputs are momentary except RHC +pitch at 00:45

Timer Jets Fired CDR PLT

-01:00 √Body rates: +0.047 ≤ roll ≤ +0.087 -0.020 ≤ pitch ≤ +0.020 -0.020 ≤ yaw ≤ +0.020

DAP: FREE DAP: A/PRI


√Forward RCS page – ITEM 1 EXEC (*)

NOTE Queue the following ITEM entry on the scratch pad. Do not perform the EXEC until specified at +00:35 sec

Queue JET DES F3D – ITEM 25

-00:30 FLT CNTLR PWR – ON 00:00 RXA, LXA THC +X (in) (3 sec firing) 00:15 FXL, LXL THC +Y (right) (3 sec firing) 00:30 FXR, RXR THC -Y (left) (3 sec firing) 00:35 When jets stop firing:

GNC 23 RCS EXEC [JET DES F3D – ITEM 25 (*)]

00:45 F4D RHC +pitch to hardstop, hold 3 sec

00:48 RHC release FLT CNTLR PWR – OFF Return to MAUI PRCS ONLY PROCEDURE,

step 6, (ORB OPS FS, P/L OF OPP)

Cont next page




Reselect Jets: JET DES F1D – ITEM 23 EXEC (no *) JET DES F3D – ITEM 25 EXEC (no *) JET DES F2D – ITEM 27 EXEC (no *)

GNC 20 DAP CONFIG


When time ≥ +02:00: √DAP: A/PRI

DAP: LVLH

When rates stable: DAP: VERN


8. RECONFIGURE TO GROUP B POWERDOWN

√MCC O14:E, cb DDU L (two) – op O15:E O14:F, Pri RJD LOGIC,DRIVER (sixteen) – OFF O15:F, RJDA 1A L2/R2 MANF DRIVER – ON O16:F


RAMBO-2 PROCEDURE

NOTE This procedure completes a Out-of-Plane, RAM, and WAKE burn in the following window: MET WINDOW OPEN: MET WINDOW CLOSE: WINDOW DURATION: Count-up pacing times from window open, prefaced with a “~”, are provided to enhance time awareness as the crew works through the procedure and will ensure completion of all burns within the window. Count-up pacing times from window open, prefaced with a “+”, are provided to indicate preferred burn TIGs for the second and third burns in the sequence (RAM and WAKE). If the vehicle arrives in attitude prior to the preferred burn time, do not deflect THC until the preferred burn time is reached on the counter; if the vehicle arrives in attitude after the preferred burn time, begin THC inputs immediately when the THC +X step is reached

-15:00 1. MANEUVER TO OOP BURN ATTITUDE or earlier GNC 20 DAP CONFIG


UNIV PTGTGT ID – ITEM 8 +2 EXEC BODY VECT – ITEM 14 +5 EXEC P – ITEM 15 + EXEC Y – ITEM 16 + EXEC OM – ITEM 17 + EXEC

DAP: A/AUTO/VERN(ALT) TRK – ITEM 19 EXEC (CUR - *)

Cont next page

ORB OPS/135/FIN 1


2. INITIATE TIMER GNC 2 TIME

Set count down/count up timer for the WINDOW OPEN time

√MET – ITEM 2 EXEC (*)

CRT TIMER COUNT TO – ITEM 17 +_ _ +_ _ +_ _ EXEC

3. SETUP O14:E, cb DDU L (two) – cl O15:E O14:F, Pri RJD LOGIC,DRIVER (sixteen) – ON O15:F, O16:F

GNC 20 DAP CONFIGDAP B PRI ROT RATE – ITEM 30 +1.0 0 EXEC DAP B PRI ATT DB – ITEM 31 +5 EXEC DAP B PRI P OPTION – ITEM 35 EXEC (NOSE) DAP B PRI Y OPTION – ITEM 36 EXEC (NOSE)

DAP TRANS: NORM/PULSE/PULSE

4. VERIFY OOP BURN ATTITUDE

-01:00 Verify in attitude F6 FLT CNTLR PWR – ON -00:20 DAP: B/AUTO/PRI

5. OOP BURN 0:00 THC +X (in) for 10 seconds F6 FLT CNTLR PWR – OFF

Wait 20 seconds before executing the next maneuver or changing the DAP configuration



6. RAM BURN MANEUVER UNIV PTG

P – ITEM 15 + EXEC Y – ITEM 16 + EXEC OM – ITEM 17 + EXEC

DAP: B/AUTO/ALT

~00:35 TRK – ITEM 19 EXEC (CUR - *) When in attitude with rates <0.2 deg/sec:

DAP: B/VERN

Wait 5 seconds: DAP: B/PRI

Wait 20 seconds before THC inputs

7. RAM BURN

F6 FLT CNTLR PWR – ON

NET +03:00 THC +X (in) for 10 seconds

F6 FLT CNTLR PWR – OFF

Wait 20 seconds before executing the next maneuver or changing the DAP configuration

8. WAKE BURN MANEUVER

UNIV PTG

P – ITEM 15 + EXEC Y – ITEM 16 + EXEC OM – ITEM 17 + EXEC

DAP: B/AUTO/ALT

~03:35 TRK – ITEM 19 EXEC (CUR - *) When in attitude with rates <0.2 deg/sec:

DAP: B/VERN



Wait 5 seconds: DAP: B/PRI

Wait at least 20 seconds before THC inputs

9. WAKE BURN

F6 FLT CNTLR PWR – ON NET +06:00 THC +X (in) for 10 seconds F6 FLT CNTLR PWR – OFF

10. CLEAN UP Wait 20 seconds before returning to VERN(ALT) below or executing a maneuver

GNC 20 DAP CONFIG

DAP B1 – ITEM 2 +1 EXEC

DAP TRANS: PULSE/PULSE/PULSE DAP: A/VERN(ALT)


11. RECONFIGURE TO GROUP B POWERDOWN MCC

O14:E, cb DDU L (two) – op O15:E O14:F, Pri RJD LOGIC,DRIVER (sixteen) – OFF O15:F, RJDA 1A L2/R2 MANF DRIVER – ON O16:F

ORB OPS/135/FIN 1


CWC OPS

WASTE TANK OFFLOAD TO CWC .............................. FS 9-2

CW

C O

PS


WASTE TANK OFFLOAD TO CWC

OBJECTIVE: Use CWC to temp store waste water in the event the waste tank is full and cannot be dumped. CWC will be dumped at a later time

NOTE Requires Ops 2 config and two crewmembers

LOCATION: CONT H2O X-TIE WASTE QD located on outboard WCS wall (inside WCS compartment), Volume H (MD23R); see LOWER EQUIPMENT BAY (IFM, COMPONENT LOCATIONS)

TOOLS REQD: TOOL Gray Tape CHCK 8 ft Y-Y Hose WCS Dry Wipes (2-3) MISC PPE (gloves and goggles) 36 x 36 Ziploc Bag (two) Middeck Contingency Water Container (CWC) (Check MCC for CWC S/N) 1. Remove contents of Vol H (MD23R), temp stow 2. Connect Y-Y Hose to CWC 3. Place CWC in one Ziploc ML31C 4. WASTE H2O DUMP ISOL VLV – CL (tb-CL)

NOTE Discontinue WCS ops until procedure complete. Use Dry Wipes to absorb any fluid released during QD mate/demate

5. Don PPE WCS 6. Connect Y-Y Hose to CONT H2O X-TIE WASTE QD

(upper QD with yellow Velcro and “WASTE” label) NOTE

MCC will TMBU limits if desired

Cont next page

CW

C O

PS


7. FDA limit for Waste TK to CWC transfer _____% 8. SM 60 TABLE MAINT

PARAMETER NAME

PARA ID SM ALERT LOW HIGH

WASTE H2O QTY 1 0620540 - ML31C 9. WASTE H2O DUMP ISOL VLV – OP (tb-OP) 10. Monitor CWC fill rate continuously SM 66 ENVIRONMENT 11. When ‘S66 WASTE H2O QTY ↓’, continue ML31C 12. WASTE H2O DUMP ISOL VLV – CL (tb-CL) WCS 13. Leave Y-Y Hose connected to CWC, disconnect Y-Y

Hose from CONT H2O X-TIE WASTE QD, cap QD ML31C 14. WASTE H2O DUMP ISOL VLV – OP (tb-OP) 15. Leaving Y-Y Hose protruding from corner of bag,

lightly press air out of Ziploc, seal bag 16. Use Gray Tape to seal area around location where

Y-Y Hose exits Ziploc (see photo below)

Cont next page


17. Fold any extra portion of Ziploc flat, coil Y-Y Hose on top

18. Place bagged CWC/Y-Y Hose assembly into second

Ziploc , lightly press air out of bag, seal Ziploc 19. Temp stow entire assembly in Vol H (MD23R),

ensuring minimal pressure is applied to CWC 20. Stow tools


PGSC FS

KFX DOWNLINK IN THE BLIND ................................... FS 10-2

PGSC

FS


KFX DOWNLINK IN THE BLIND

1. Verify with MCC that the KFX application is running on the OCA PLAN A client and that the MCC is configured for an OCA Downlink

2. CONFIGURE KFX APPLICATION

PGSC If reqd, enlarge KFX window

On KFX menu bar select ‘View’>‘Options’ In ‘Options’ window click ‘Network’ tab In ‘Network’ tab change ‘Maximum Xmit Rate’ to ‘1500’ Kbits/sec

Click ‘OK’ Click ‘Yes’ when prompted for KFX S/W restart

After KFX S/W restart, on ‘KFX’ window: √REMOTE KFX – yellow √Uplink arrow (‘↑’ next to send rate) – yellow √Dnlink arrow (‘↓’ next to send rate) – yellow

3. SELECT FILE(S) TO DOWNLINK

Use WINDOWS EXPLORER to sel files/directories to transfer

Drag files over KFX window Rel mouse button

The following dialog will be displayed when the files for downlink are dragged over the KFX window:

Click ‘OK’

√‘KFX File Transfer Preview’ display appears with selected file(s) listed

Cont next page

PGSC

FS


4. ADD ADDITIONAL FILE FOR DOWNLINK (if reqd) √‘KFX File Transfer Preview’ display active

Sel ‘add to list’ button (button with documents, ‘+’ symbols)

√‘Select Files from Transfer’ display appears Sel desired file from file listbox Sel ‘Select’ button Repeat for each additional file as reqd Sel ‘Done’ button

5. REMOVE FILE FROM DOWNLINK (if reqd) √‘KFX File Transfer Preview’ display active

Sel desired file(s) in listbox Sel ‘delete’ button (button with ‘X’)

6. START FILE DOWNLINK

NOTE

User may halt transfer while in progress by sel ‘Abort’ button

√‘KFX File Transfer Preview’ display active

Sel ‘downlink’ button (button with ‘↓’)

The following two warning dialogs will be displayed:

Click ‘Yes’

Cont next page


On MCC Go, click ‘Ignore’ √‘File Transfer Status’ display appears √Displaying xfer status

* If error displayed, repeat step 6 *

NOT FLOWN FS 11-1 ORB OPS/135/FIN

CUE CARD CONFIGURATION

CU

E C

AR

DS



CU

E C

AR

DS

NOT FLOWN FS CC 11-3 ORB OPS/135/FIN

HOOK VELCRO

LIOH CHANGEOUT (4 crewmembers/Single Shift/FD 1-16)

FLIGHT DAY POS A POS B CK CMPLTLAUNCH 1 2 PRE FD01 " " POST FD02 3 " PRE FD02 " 4 POST FD03 5 " DOCKING

PRE FD03 " 6 POST FD04 " " PRE FD04 7 "POST FD05 " " EVA 1

PRE FD05 " STS-132 42POST FD06 " " PRE FD06 STS-133_____ " POST FD07 " " PRE FD07 " STS-133_____POST FD08 " " PRE FD08 STS-133_____ " POST FD09 " " PRE FD09 " STS-133_____POST FD10 " " MID FD10 STS-133____* STS-133_____ HATCH CLOSE

PRE FD10 " "POST FD11 STS-133_____ " UNDOCKING

PRE FD11 " STS-133_____POST FD12 STS-133_____ " PRE FD12 " STS-133_____POST FD13 STS-133_____ " EOM

PRE FD13 " 20 POST FD14 21 " EOM+1



* Re-bag and seal LiOH cans with Gray Tape and stow (Location of canisters on back)

NOTE This card is specifically used for the STS-135 mission with the Orbiter conducting single shift operations with a crew size of 4. This changeout scheme reflects FD3 docking with ISS, Vozdukh, and dual-bed CDRA operation.

TOP

ORB OPS-29a/nonRCRS/135/O/B

(reduced copy) ORB OPS/135/FIN 1


HOOK VELCRO

LIOH CANISTER STOWAGE LOCATIONS

Ascent Stowage Locations

Orbiter: MD52M (LiOH Box): Cans 1-31 *

ISS: Pregathered: STS-132 Can 42

STS-133 Cans 8-18 STS-134 Cans 1-6 (Used)

Entry Stowage Locations

Orbiter: MD52M (LiOH Box): STS-135 Cans 1-7 and 20-25

STS-132 Can 42 STS-133 Cans 8-18 STS-134 Cans 1-6 (Used)

ISS: STS-135 cans 8-19 and 26-31

* Two LiOH cans installed in LiOH slots A and B

TOP BACK OF ‘LIOH CHANGEOUT’

ORB OPS-29b/nonRCRS/135/O/B

(reduced copy) ORB OPS/135/FIN 1


ORBIT BURN MONITOR

OMS TEMP* FU IN P ≥ ≤ or No FU IN P

OMS ENG FAIL OMS PRPLT FAIL

OMS PC* & OMS ↓

ENG VLV 1 or 2 < 70 or OX IN P > 227 OX IN P ≤ 227 or No OX IN P

OMS ENG FAIL OMS PRPLT FAIL

OMS OX/FU TK P (√ENG IN P) OX/FU LOW He PRESS/VAP ISOL (two) – OP

If aff TK P not incr: OMS PRPLT FAIL

OX & FU HIGH He PRESS/VAP ISOL (two) – CL Cycle He A(B) to maintain TK P 234-284

OMS N2 REG P HIGH or LOW OMS ENG – ARM OMS N2 TK P LOW (√ OMS/MPS )

At N2 TK P < 470: OMS ENG – ARM

OMS GMBL PRI fail L(R) OMS GMBL – SEC SEC fail If high RCS usage: OMS ENG FAIL

GPC ( ) & aff GPC PWR – OFF Burning OMS aff If SEC GMBL avail:

aff MDM FF 1(4) – OFF,ON L(R) OMS GMBL – SEC

SEC GMBL lost If high RCS usage: OMS ENG FAIL 2 FAs lost √MAN SHUTDN

I/O ERROR FA 1(4) L(R) OMS GMBL – SEC ♦ I/O RESET

If high RCS usage: OMS ENG FAIL 2 FAs lost √MAN SHUTDN

BCE STRG D I/O RESET (if recov: >>) 1(4) If high RCS usage:

L(R) OMS GMBL – SEC GPC SET SPLIT Non-crit burn STOP BURN: OMS ENG(s) – OFF

Crit burn Go to “GPC” above I/O ERROR PCM OI PCMMU PWR – 2(1) BCE BYP OA SM I/O RESET

*If XFD, BLDN, or sensor fail, monitor ENG IN P for off-nominal performance

TOP

HOOK VELCRO

HOOK VELCRO

ORB OPS-31a/135/O/B

L R 230 230214 212

(reduced copy)


If two FA MDMs lost

MDMs Preburn: ENG – OFF

During burn: MAN SHUTDN

1,2 1,3 1,4

LEFT (TVC) RIGHT (IGN) LEFT (IGN)

BOTH LEFT RIGHT

2,3 2,4 3,4

LEFT (IGN) RIGHT (IGN) RIGHT (TVC)

RIGHT LEFT BOTH

Left OMS Pri TVC

TOP BACK OF ‘ORBIT BURN MONITOR’

HOOK VELCRO

HOOK VELCRO

ORB OPS-31b/135/O/A

OMS FAILURES

LEFT OMS

RIGHT OMS

Left OMS Sec TVC

Left OMS Ignition

MNA (ALC1)CNTLAB1 †

FA3 *

MNB (ALC2)CNTLAB2 †

FA2

MNA (APC1)FF1 FA1

MNB (APC2)FF2 FA2

MNB (ALC2) CNTLAB2 †

FA1

MNA (ALC1) CNTLAB1 †

FA4

† If CNTL AB1 or AB2 (CA1 or CA2) failed and ign path still exists at OMS fail, assume L(R) OMS ↓ is PRPLT FAIL

* If L(R) Pc failed high during burn or FA3(4) failed, at L(R) OMS fail, no guidance downmode after L(R) OMS ENG switch OFF (TGO slow, ADI needles in error, 6 ft/s underburn)

Right OMSPri TVC

Right OMSSec TVC

Right OMS Ignition

MNC (ALC3)CNTLCA1 †

FA4 *

MNA (ALC1)CNTLCA2 †

FA2

MNC (APC3)FF4 FA4 *

MNA (APC1)FF3 FA3

MNA (ALC1) CNTLCA2 †

FA1

MNC (ALC3) CNTLCA1 †

FA3

(reduced copy)

NO

T FLOW

N

FS C

C 11-7

OR

B O

PS

/135/FIN

PILE VELCRO

PILE VELCRO

ORB OPS-41a/135/O/A

HINGE

TOP



ITEM # A1 A2 A3 A4 A5 A6 A7 A8PRI

ROT RATE 10 (50) 0.2000 0.4000 0.2000 0.5000 0.2000 0.2000 0.2000 0.0500ATT DB 11 (51) 5.00 1.00 0.30 3.00 5.00 5.00 2.00 2.00RATE DB 12 (52) 0.20 0.20 0.20 0.20 0.20 0.20 0.20 0.20ROT PLS 13 (53) 0.100 0.100 0.100 0.100 0.100 0.100 0.100 0.100COMP 14 (54) .000 .000 .000 .000 .000 .000 .000 .000P OPTION 15 (55) ALL ALL ALL ALL ALL TAIL ALL ALLY OPTION 16 (56) ALL ALL TAIL ALL ALL TAIL ALL ALLTRAN PLS 17 (57) 0.100 0.100 0.100 0.100 0.100 0.100 0.100 0.100

ALT RATE DB 18 (58) 0.200 0.200 0.070 0.200 0.070 0.070 0.100 0.100JET OPT 19 (59) ALL ALL ALL ALL ALL TAIL ALL ALL# JETS 20 (60) 2 2 1 2 1 1 2 2ON TIME 21 (61) 0.08 0.08 0.08 0.08 0.08 0.08 0.08 0.08DELAY 22 (62) 0.00 0.00 0.00 0.00 0.00 0.00 0.00 0.00

VERN ROT RATE 23 (63) 0.2000 0.4000 0.0080 0.2000 0.0500 0.0500 0.0160 0.0500ATT DB 24 (64) 1.000 1.000 0.070 1.000 1.000 1.000 1.000 1.000RATE DB 25 (65) .020 .020 .010 .020 .020 .020 .020 .020ROT PLS 26 (66) 0.010 0.010 0.010 0.010 0.010 0.010 0.010 0.050COMP 27 (67) .000 .000 .000 .000 .000 .000 .000 .000CNTL ACC 28 (68) 0 0 0 0 0 0 0 0PURPOSE NOMINAL PTC GG LOSS OF

VERN (ALL) LOSS OF

VERN (TAIL ONLY)

RNDZ TERMINAL PHASE

(reduced copy)

NO

T FLOW

N

FS C

C 11-8

OR

B O

PS

/135/FIN

HINGE

HOOK VELCRO

HOOK VELCRO

TOPHINGED AT BOTTOM OF

‘STS-135 DAP A1 – DAP A8 CONFIGURATIONS’

ORB OPS-41aa/135/O/A

STS-135 DAP B1 – DAP B8 CONFIGURATIONSITEM # B1 B2 B3 B4 B5 B6 B7 B8

PRI ROT RATE 30 (50) 0.5000 0.2000 0.2000 0.2000 0.2000 0.5000 0.5000 0.0500ATT DB 31 (51) 3.00 3.00 3.00 0.30 3.00 3.00 2.00 2.00RATE DB 32 (52) 0.20 0.20 0.20 0.20 0.20 0.20 0.20 0.20ROT PLS 33 (53) 0.040 0.040 0.040 0.040 0.040 0.040 0.040 0.040COMP 34 (54) .000 .000 .000 .000 .000 .000 .000 .000P OPTION 35 (55) ALL TAIL ALL TAIL TAIL ALL ALL ALLY OPTION 36 (56) ALL TAIL ALL TAIL TAIL ALL ALL ALLTRAN PLS 37 (57) 0.100 0.020 0.020 0.020 0.020 0.020 0.050 0.050

ALT RATE DB 38 (58) 0.200 0.070 0.070 0.100 0.200 0.200 0.100 0.100JET OPT 39 (59) ALL TAIL ALL ALL ALL ALL ALL ALL# JETS 40 (60) 2 1 1 2 2 2 2 2ON TIME 41 (61) 0.08 0.08 0.08 0.08 0.08 0.08 0.08 0.08DELAY 42 (62) 0.00 0.00 0.00 0.00 0.00 0.00 0.00 0.00

VERN ROT RATE 43 (63) 0.2000 0.2000 0.2000 0.0080 0.0160 0.2000 0.2000 0.0500ATT DB 44 (64) 1.000 1.000 1.000 0.100 0.033 1.000 1.000 1.000RATE DB 45 (65) .020 .020 .020 .010 .020 .020 .020 .020ROT PLS 46 (66) 0.002 0.002 0.002 0.002 0.002 0.002 0.002 0.020COMP 47 (67) .000 .000 .000 .000 .000 .000 .000 .000CNTL ACC 48 (68) 0 0 0 0 0 0 0 0PURPOSE OMS & RCS

BURNS (ORB OPS)

LOSS OF VERN

(TAIL ONLY)

LOSS OF VERN (ALL)

COAS/HUD CAL

RNDZ TERMINAL PHASE


(reduced copy)

NO

T FLOW

N

FS C

C 11-9

OR

B O

PS

/135/FIN

PILE VELCRO

PILE VELCRO

ORB OPS-41b/135/O/B

HINGE

TOPBACK OF ‘STS-135 DAP A1 – DAP A8 CONFIGURATIONS’


BOLD/ITALIC indicates change from I-Load.1 I-loaded below keyboard limit; do not change 2 CA2 – Light Weight Russian Segment 2 CA4 – Medium Weight Russian Segment 2 CA6 – Heavy Weight Russian Segment 3 Use 1 for OBSS scan and 2 for Orbiter attitude maneuvers

ITEM # A9 A10 A11 A12 A13 A14PRI

ROT RATE 10 (50) 0.1300 0.0500 0.0500 0.0500 0.0500 0.2000ATT DB 11 (51) 2.00 0.60 10.00 5.00 5.00 5.00RATE DB 12 (52) 0.10 0.10 0.20 0.20 0.20 0.20ROT PLS 13 (53) 0.100 0.100 0.100 0.040 0.040 0.100COMP 14 (54) .000 .000 .000 .000 .000 .000P OPTION 15 (55) TAIL TAIL TAIL TAIL TAIL TAILY OPTION 16 (56) TAIL TAIL TAIL TAIL TAIL TAILTRAN PLS 17 (57) 0.050 0.050 0.100 0.010 0.010 0.100

ALT RATE DB 18 (58) 0.100 0.100 0.020 1 0.020 1 0.020 1 0.200JET OPT 19 (59) TAIL TAIL TAIL TAIL TAIL TAIL# JETS 20 (60) 2 2 1 1 1 1(2) 3 ON TIME 21 (61) 0.08 0.08 0.08 0.08 0.08 0.08DELAY 22 (62) 0.00 0.00 5.00 5.00 5.00 6.00

VERN ROT RATE 23 (63) 0.1300 0.0500 0.1000 0.1000 0.1000 0.2000ATT DB 24 (64) 1.000 0.500 5.000 3.000 3.000 3.000RATE DB 25 (65) .020 .020 .050 .020 .020 .200ROT PLS 26 (66) 0.050 0.050 0.010 0.002 0.002 0.010COMP 27 (67) .000 .000 .000 .000 .000 .000CNTL ACC 28 (68) 0 0 6(2,4) 2 6(2,4) 2 6(2,4) 2 1PURPOSE PROX/OPS

FLYAROUND DOCKING AUTO

REBOOST MATED STACK

(MNVRS, ROBO,ATT HOLD)

ORBITERALONE

SRMS/OBSS

(reduced copy)

NO

T FLOW

N

FS C

C 11-10

OR

B O

PS

/135/FIN

HINGE

HOOK VELCRO

HOOK VELCRO

TOPBACK OF ‘STS-135 DAP B1 – DAP B8 CONFIGURATIONS’

HINGED AT BOTTOM OF ‘STS-135 DAP A9 – DAP A14 CONFIGURATIONS’

ORB OPS-41bb/135/O/B


BOLD/ITALIC indicates change from I-Load.1 I-loaded below keyboard limit; do not change 2 CA2 – Light Weight Russian Segment 2 CA4 – Medium Weight Russian Segment 2 CA6 – Heavy Weight Russian Segment

ITEM # B9 B10 B12 B13PRI

ROT RATE 30 (50) 0.1300 0.0500 0.0100 1 0.0100 1

ATT DB 31 (51) 2.00 0.60 1.00 1.00RATE DB 32 (52) 0.10 0.10 0.20 0.20ROT PLS 33 (53) 0.040 0.040 0.040 0.040COMP 34 (54) .000 .000 .000 .000P OPTION 35 (55) TAIL TAIL TAIL TAILY OPTION 36 (56) TAIL TAIL TAIL TAILTRAN PLS 37 (57) 0.010 0.010 0.010 0.010

ALT RATE DB 38 (58) 0.100 0.100 0.020 1 0.020 1 JET OPT 39 (59) TAIL TAIL TAIL TAIL# JETS 40 (60) 2 2 1 1ON TIME 41 (61) 0.08 0.08 0.08 0.08DELAY 42 (62) 10.00 0.00 5.00 5.00

VERN ROT RATE 43 (63) 0.1300 0.0500 0.0100 0.0100ATT DB 44 (64) 1.000 0.500 1.000 0.100RATE DB 45 (65) .020 .020 .020 .020ROT PLS 46 (66) 0.020 0.020 0.002 0.002COMP 47 (67) .000 .000 .000 .000CNTL ACC 48 (68) 0 0 6(2,4) 2 6(2,4) 2 PURPOSE PROXOPS/

FLYAROUND DOCKING MATED

ATT HOLD (VRCS & ALT)

MATED VRCS DB COLLAPSE

(reduced copy)


MAUI PRCS AND VRCS – RCS FIRING SEQUENCE Reminder: All inputs are momentary


+0.047 ≤ roll ≤ +0.087 -0.020 ≤ pitch ≤ +0.020 -0.020 ≤ yaw ≤ +0.020

DAP: FREE DAP: A/PRI Inform PLT “GO” for jet deselects


Left RCS page – ITEM 2 EXEC On CDR “GO”, proceed


Deselect jets: JET DES L5L – ITEM 37 EXEC (*) Right RCS page – ITEM 3 EXEC JET DES R5D – ITEM 39 EXEC (*) Forward RCS page – ITEM 1 EXEC JET DES F5L – ITEM 37 EXEC (*)

-00:30 FLT CNTLR PWR – ON 00:00 RXA, LXA THC +X (in) (3 sec firing) 00:15 FXL, LXL THC +Y (right) (3 sec firing) 00:30 FXR, RXR THC -Y (left) (3 sec firing) 00:35 DAP: VERN 00:45 R5R RHC +yaw (10 sec firing)




FLT CNTLR PWR – OFF Return to MAUI PRCS AND VRCS PROCEDURE, step 6, (ORB OPS FS, P/L OF OPP)

ORB OPS-42a/135/O/A

TOP

HIN

GE

PILE VELCRO

PILE VELCRO

(reduced copy)


MAUI PRCS ONLY FIRING SEQUENCEReminder: All inputs are momentary except RHC +pitch at 00:45


+0.047 ≤ roll ≤ +0.087 -0.020 ≤ pitch ≤ +0.020 -0.020 ≤ yaw ≤ +0.020

DAP: FREE DAP: A/PRI


√Forward RCS page – ITEM 1 EXEC (*)

NOTE Queue the following ITEM entry on the scratch pad. Do not perform the EXEC until specified at +00:35 sec

Queue JET DES F3D – ITEM 25

-00:30 FLT CNTLR PWR – ON 00:00 RXA, LXA THC +X (in) (3 sec firing) 00:15 FXL, LXL THC +Y (right) (3 sec firing) 00:30 FXR, RXR THC -Y (left) (3 sec firing) 00:35 When jets stop firing:

GNC 23 RCS EXEC [JET DES F3D – ITEM 25 (*)]

00:45 F4D RHC +pitch to hardstop, hold 3 sec

00:48 RHC release FLT CNTLR PWR – OFF Return to MAUI PRCS ONLY PROCEDURE,

step 6, (ORB OPS FS, P/L OF OPP)

ORB OPS-42aa/135/O/A

TOP BACK OF ‘ MAUI PRCS AND VRCS - RCS FIRING SEQUENCE

HIN

GE

PILE VELCRO

PILE VELCRO

HOOK VELCRO

HOOK VELCRO

HOOK VELCRO

(reduced copy)


MAUI VRCS ONLY FIRING SEQUENCEReminder: All inputs are momentary


-0.020 ≤ roll ≤ +0.020 -0.087 ≤ pitch ≤ -0.047 -0.020 ≤ yaw ≤ +0.020

DAP: FREE √DAP: VERN Inform PLT “GO” for jet deselects


Left RCS page – ITEM 2 EXEC (*) On CDR “GO”, proceed


Deselect jets: JET DES L5L – ITEM 37 EXEC (*) Right RCS page – ITEM 3 EXEC (*) JET DES R5D – ITEM 39 EXEC (*) Forward RCS page – ITEM 1 EXEC (*) JET DES F5L – ITEM 37 EXEC (*)

-00:30 FLT CNTLR PWR – ON 00:00 R5R RHC +yaw (10 sec firing)




FLT CNTLR PWR – OFF Return to MAUI VRCS ONLY PROCEDURE, step 6, (ORB OPS FS, P/L OF OPP)

ORB OPS-42b/135/O/A

TOP

HIN

GE

HIN

GED

TOR

IGH

TSID

EO

F‘M

AUIPR

CS

ON

LYFIR

ING

SEQ

UEN

CE

’

HOOK VELCRO

HOOK VELCRO

HOOK VELCRO

HOOK VELCRO

(reduced copy)


HOOK VELCRO

HOOK VELCRO

HOOK VELCRO

HOOK VELCRO

HIN

GE

HIN

GE

TOLE

FTSI

DE

OF

‘MAU

IPR

CS

AND

VRC

S-R

CS

FIR

ING

SEQ

UEN

CE’

ORB OPS-42bb/135/O/A

TOP BACK OF ‘MAUI VRCS ONLY FIRING SEQUENCE’

(reduced copy)


WLES CONFIG AFTER PGSC REBOOT 1. If window appears asking to launch WLES software:

Click ‘1’ to launch WLES software Else:

Double click ‘Shuttle Apps’>‘WLES’>‘WLES’ 2.√MCC for ‘Backup Mode Selection’ 3. If ‘EWBMTAU-WLEFlight’ appears with message ‘Run

the current command: XXXX_AA_BB_SNYYYY.xml?’: Click ‘Yes’

FABRICATION NOTES Fabricated as a decal (SED33112142)

ORB OPS-47a/135/O/A

TOP

(reduced copy)

Flight Cover (trim bottom to expose tabs)

JSC-48036-135 FINAL

ORBIT OPS CHECKLIST

STS

135

orbit operations checklist - nasafs iii orb ops/135/fin 1 orbit operations checklist sts-135 flight...

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